WO2019179701A1

WO2019179701A1 - Rotor blade monitoring system

Info

Publication number: WO2019179701A1
Application number: PCT/EP2019/053760
Authority: WO
Inventors: Donato GIROLAMO; Esben Orlowitz; Nevena Stevanovic
Original assignee: Siemens Gamesa Renewable Energy A/S
Priority date: 2018-03-22
Filing date: 2019-02-15
Publication date: 2019-09-26
Also published as: EP3749855A1; US20210071647A1; EP3543522A1; EP3749855B1; ES2911300T3; CN111868376A; DK3749855T3

Abstract

It is described a rotor blade (220, 320, 420, 520, 620, 720) for a wind turbine (760), comprising: at least one camera (101) mounted inside the rotor blade and adapted to acquire an image of a portion of an inner surface (219) of the rotor blade (220).

Description

DESCRIPTION

Rotor blade monitoring system

Field of invention

The present invention relates to a rotor blade for a wind turbine, relates to a rotor blade monitoring system, relates to a wind turbine and further relates to a method of monitor ing a structural state of a rotor blade of a wind turbine.

Art Background

A wind turbine may comprise a rotation shaft with a hub at which plural rotor blades are mounted. The rotation shaft may mechanically be coupled with a rotor of a generator to gener ate electric energy upon rotation of the hub to which the ro tor blades are connected. The rotor blades may be subject to wear during operation such that they deteriorate over pro longed operation time.

Therefore, monitoring the structural state or structural in tegrity of the rotor blades is necessary. Monitoring of the structural health of the wind turbine blades may convention ally require regular in-situ inspection, in order to avoid critical failure modes of the blades structure. In-situ in spection of blades on wind turbines however is currently costly and time-consuming. Furthermore, it may be weather- dependent and often the wind turbines are situated in hard- to-access sites in remote areas or offshore installations, making it difficult to plan and perform inspections. Addi tionally, the rotor blades nowadays are relatively large and expensive components of wind turbines. Thus, a lengthy struc tural repair involving stopped energy production or blade loss due to structural damage may involve major disad

vantages . Conventional visual in-situ inspection is performed by maintenance personnel on a yearly or biyearly basis for all wind turbines of a wind park. Thereby, maintenance personnel enters the blades, inspects the surfaces and takes pictures if suspicious observations are found. This monitoring opera tion can be done only one blade at a time because the blade under inspection needs to be horizontal which again may put requirements on the weather condition. The decision if damage is present is subjectively judged by a person and the end re sult will depend on that person's knowhow and experience.

Thus, there may be a need for a rotor blade for a wind tur bine, for a rotor blade monitoring system, for a wind turbine and further for a method of monitoring a structural state of a rotor blade of a wind turbine, wherein monitoring can be performed in a simplified manner and in a reliable manner, in particular without requiring that maintenance personnel is present .

Summary of the Invention

This need may be met by the subject matter according to the independent claims. Advantageous embodiments of the present invention are described by the dependent claims.

According to an embodiment of the present invention it is provided a rotor blade for a wind turbine, comprising: at least one camera mounted inside the rotor blade and adapted to acquire an image of a portion of an inner surface of the rotor blade.

The camera may be adapted to acquire one or more two- dimensional images of the portion of the inner surface of the rotor blade. Therefore, the camera may comprise plural light- sensitive elements for example arranged in a two-dimensional array. The light-sensitive elements may for example comprise a CCD or a CMOS unit. The camera (s) may also comprises one or more optical filters that filter out one or more spectral ranges, such as a visible range, infrared light range, ultra violet range, and thereby allow to form the images by acquir ing intensities of selected wavelength range (s). Further one or more lenses or in general an objective may be arranged in front of the light sensitive elements, allowing focussing.

The camera may be permanently mounted inside the rotor blade such that the camera is also mounted within the rotor blade while the wind turbine is in normal operation, thus producing electric energy upon rotation of the rotor blades. Depending on the extent of the rotor blade and the viewing ranges (e.g. angles) of the camera, plural cameras may be mounted inside the rotor blade and mounted at different positions such that they are enabled to essentially acquire images of the entire inner surface of the rotor blade. Thereby, it may be avoided that maintenance personnel enters inside the rotor blade and manually takes pictures of critical regions of the inner sur face .

The rotor blade may have an (internal) hollow space with at least one shear web. The shear web (or web) may be an inter nal structural subcomponent of the rotor blade. It connects the spar caps present at the pressure and suction sides and may have the function of transferring the shear loads that are present in the blade due to the flapwise bending moment applied to the structure. It may consist of or comprise a composite sandwich plate having plywood core and glass fiber reinforced plastic (GFRP) facesheets.

The camera may be mounted directly or indirectly at a mount ing portion of the inner surface, for example by gluing a mounting face of the camera or a mounting face of a frame at which the camera is mounted to the mounting portion of the inner surface. The camera may also be bolted to the inside of the rotor blade or may be mounted by other means. Thereby, simple monitoring of the structural state of the blade may be enabled . According to an embodiment of the present invention, the ro tor blade further comprises at least one light source mounted inside the rotor blade, adapted to generate illumination light and arranged to illuminate the portion of the inner surface .

Other embodiments of the present invention may not require a light source, since light from the environment may enter the inside of the rotor blade, for example in cases where the ro tor blade wall is at least partly transparent. However, to more accurately control the brightness, the light source may be advantageous to accurately adjust brightness of the illu minated portion of the inner surface and/or adjust an image acquisition time of the camera to acquire at least one image. Using for example a control module or the like, the at least one light source may be controllable regarding switching on and off the light source and/or also regarding adjusting the brightness of the light source or the intensity of the light source. For example, a control module may be adapted to con trol the light source to switch the light source on only if acquiring at least one image is desired for monitoring the rotor blade. For example, at least one image may be taken on a regular time basis, such as daily, every two days, every week, three times a month or yearly, for example. During these periods of image acquisitions, the light source may be controlled to be switched on. The illumination light may com prise at least visible light (for example from about 300 nm to about 800 nm) and/or may at least comprise one or more wavelength ranges within the visible light spectrum. Further, the illumination light may comprise or may not comprise in frared light (or at least some wavelength range of the infra red spectrum) and/or ultraviolet light or ultraviolet wave length ranges. Having an appropriate illumination by the light source may improve the image quality.

According to an embodiment of the present invention, the at least one camera and/or the at least one light source is mounted at a mounting portion of the inner surface, wherein the at least one camera and/or the at least one light source is in particular mounted using an adhesive.

The inner surface may be a surface of a rotor blade wall providing at the outside an airfoil at which the wind im pacts. The airfoil is shaped to cause the rotor blade to ex ert a momentum to the rotation shaft in order to effect a ro tation of the rotation shaft. When the camera and/or the light source is mounted at a mounting portion of the inner surface, no particular provision of a particular mounting ar rangement may be necessary, but the camera and/or the light source may be plainly mounted at the inner surface which is unmodified compared to a conventional inner surface of a ro tor blade.

When an adhesive is used, the shape of the outer surface (in particular forming an airfoil) of the rotor blade may not be altered or effected. Thereby, the aerodynamic property of the rotor blade may be unchanged. The adhesive may for example be or comprise a polymer resin which has been hardened, thereby forming a cross-linked polymer. Also the rotor blade wall (having the inner surface and the outer airfoil) may be manu factured from a polymer which has been cross-linked. Other manufacturing materials and methods are possible. Thereby, mounting the camera and/or the light source at conventionally utilized rotor blade materials may be enabled.

According to an embodiment of the present invention, the at least one camera and/or the at least one light source is mounted on at least one frame that is mounted on the inner surface. The frame may enable to properly adjust the orienta tion of the camera and/or the light source such that the light source illuminates a region of the inner surface which is also in the viewing range of the camera. Further, the frame may enable to properly adjust the orientation and posi tioning of the camera and/or the light source such that the camera does not shadow the illumination light, is not in the illumination light path. The frame may have mounted thereon one camera, two cameras, three cameras or even more cameras and one light source, two light sources, three light sources or even more light sources.

According to an embodiment of the present invention, the frame has a mounting surface which is fit, in particular com plementary, to a shape of the mounting portion of the inner surface. When the mounting surface of the frame is complemen tary to the shape of the mounting portion of the inner sur face, the mounting surface may in a simple manner be glued to the mounting portion of the inner surface, thereby simplify ing mounting the frame to the inside of the rotor blade.

Providing the frame may allow to utilize conventionally available cameras and light sources without requiring the cameras and the light sources to have particularly shaped mounting surfaces, since the frame may serve as an adaptor. Thereby, costs may be reduced. The frame may be made of any material, such as a polymer, a metal, wood, any plastic, any thermosetting material, or the like. In particular, differ ently shaped frames regarding their mounting surface may be utilized having respective mounting surfaces which are com plementary to different mounting portions of the inner sur face, for example along the longitudinal direction of the ro tor blade.

According to an embodiment of the present invention, the at least one camera comprises plural cameras mounted inside the rotor blade and adapted to acquire plural images of plural, in particular partly overlapping, portions of the inner sur face of the rotor blade, and/or wherein the light source com prises plural light sources mounted inside the rotor blade and arranged to illuminate the plural portions of the inner surface .

Having plural cameras and/or plural light sources may enable to essentially monitor the entire inner surface of the rotor blade . In other embodiments the at least one camera comprises exact ly one camera, in particular having large viewing angle cov ering 180°.

According to an embodiment of the present invention, at least one image acquisition unit is formed by an assembly of at least one camera, in particular three cameras, at least one light source all mounted on one frame, wherein the rotor blade in particular comprises plural image acquisition units, further in particular arranged in sets of image acquisition units mounted to face each other.

Providing at least one image acquisition unit may simplify the construction and reduce costs. Inside the rotor blade, one image acquisition unit may be mounted on for example a back side of a luv outer surface of the rotor blade and an other image acquisition unit may be oppositely mounted inside the rotor blade at a back side of a lee outer surface of the rotor blade. Thereby, a set of acquisition units is formed. Several sets of image acquisition units may be mounted inside the rotor blade for example spaced apart along a longitudinal direction of the rotor blade.

According to an embodiment of the present invention, cameras on one image acquisition unit: are oriented to have viewing directions differing by at least 20°, in particular by be tween 25° and 70°, further in particular by between 35° and 40°, and/or mounted close to each other such as to enable ac quiring images from the entire surface of interest.

In particular, on one image acquisition unit, three or e.g. six cameras may be provided having the different viewing di rections. The three cameras may simultaneously or successive ly acquire respective images and the images may be stitched together resulting in a combination image comprising infor mation of essentially 180° or an entire back side of a lee outer side or luv outer side of the rotor blade. In other em bodiments, only one camera may be present in an image acqui- sition unit having a viewing angle of between 170° and 180° for example.

According to an embodiment of the present invention, the mounting portion of the inner surface is a back surface of an airfoil portion of the blade. The airfoil portion may be a portion of a lee side or a luv side of the rotor blade.

According to an embodiment of the present invention, the plu ral portions of the inner surface essentially cover an entire longitudinal extent of the blade. Thereby, a thorough moni toring of the rotor blade may be enabled.

According to an embodiment of the present invention, the at least one camera is sensitive to at least a portion of visual light and/or to at least a portion of infrared light and/or to at least a portion of ultraviolet light.

Also the light source may be adapted to generate visible light and/or may be adapted to generate at least a portion of ultraviolet light and/or a portion of infrared light. Depend ing on the kind of damage to be identified, using different wavelength ranges may be advantageous.

According to an embodiment of the present invention, the ro tor blade further comprises a wireless or wire based communi cation interface for communicating control signals and/or im age data between the at least one camera and/or the at least one light source and a control module outside the rotor blade. Further, electrical energy may be supplied to the blade monitoring system from outside the rotor blade.

For example, using control signals from an external (or in ternal) control module, the camera and/or the light source may be controlled to be switched on or off or may be config ured regarding generated light intensity or brightness or re garding image acquisition time, focusing, applying filters or the like. The camera (or a processing module within the rotor blade) may be enabled to perform some pre-processing, for ex ample performing averaging, filtering, feature extraction or the like. The wire based communication interface may be adapted for an electrical wire and/or an optical wire.

According to an embodiment it is provided a rotor blade moni toring system, comprising: a rotor blade according to any of the preceding embodiments; and an analysis module comprising image processing capability to process the image to recognize features in the image indicating damage of the inner surface.

The analysis module may have access to a library of reference images which may be compared to the images acquired by the camera within or inside the rotor blade, in order to detect faults or damage. Any electronics (e.g. comprised in the analysis module) may be encloses in a proper casing for pro tection of the electronics, the cases e.g. providing a par ticular IP rating.

According to an embodiment of the present invention it is provided a wind turbine comprising: a rotation shaft; and a rotor blade according to any of the preceding embodiments or a rotor blade monitoring system according to the preceding embodiment, wherein the rotor blade is mounted at the rota tion shaft.

It should be understood, that features, individually or in any combination, disclosed, described or explained in the context of a rotor blade or a rotor blade monitoring system or a wind turbine may also be applied, individually or in any combination, to a method of monitoring a structural state of a rotor blade of a wind turbine and vice versa according to embodiments of the present invention.

According to an embodiment of the present invention it is provided a method of monitoring a structural state of a rotor blade of a wind turbine, the method comprising: using at least one camera mounted inside the rotor blade to acquire at least one image of a portion of an inner surface of the rotor blade; and analysing the image to determine the structural state of the rotor blade.

The aspects defined above and further aspects of the present invention are apparent from the examples of embodiment to be described hereinafter and are explained with reference to the examples of embodiment. The invention will be described in more detail hereinafter with reference to examples of embodi ment but to which the invention is not limited.

Brief Description of the Drawings

Fig. 1 schematically illustrates an image acquisition unit which may be installed in a rotor blade according to an em bodiment of the present invention;

Fig. 2 schematically illustrates viewing angles of cameras of an image acquisition unit as configured according to an em bodiment of the present invention;

Fig. 3 schematically illustrates in a perspective view an ar rangement of two image acquisition units within a rotor blade according to an embodiment of the present invention;

Figs. 4, 5 and 6 schematically illustrate further arrange ments of image acquisition units within a rotor blade accord ing to embodiments of the present invention;

Fig. 7 illustrates a method scheme of a method for monitoring a rotor blade according to an embodiment of the present in vention; and

Fig. 8 schematically illustrates a wind turbine according to an embodiment of the present invention. Detailed Description

The illustration in the drawings is in schematic form. It is noted that in different figures, similar or identical ele ments are provided with the same reference signs or with ref erence signs, which are different from the corresponding ref erence signs only within the first digit.

According to an embodiment of the present invention, multi ple, permanent mounted camera sensors are regularly (e.g. at regular time intervals) taking pictures covering the full in ternal surface of the rotor blade from the root start to the end of the web start. The camera sensors may be collected in units together with a light source, for example as is illus trated in a schematic form in Fig. 1.

Thereby, Fig. 1 illustrates an image acquisition unit 100 that may be installed inside a rotor blade according to an embodiment of the present invention. Thereby, the image ac quisition unit 100 comprises an assembly of at least one cam era 101, at least one light source 103 and a mounting frame 105 at which the camera 101 and the light source 103 are mounted. Furthermore, the mounting frame or frame 105 com prises a mounting plate 107 having a mounting surface 109 which may directly be attached, for example by gluing, to an inner surface of a rotor blade.

The image acquisition unit 100 may comprise more than one cameras 101, such as two cameras, three cameras or even more cameras which may be oriented to direct their respective viewing ranges in different angle ranges. The camera 101 may comprise an imaging optics (optionally including spectral filter (s) ) and an array of light-sensitive elements, such as a two-dimensional CCD array or CMOS array, for example.

The mounting frame 105 comprises component mounting areas 111 comprising threaded holes at which components, such as the camera 101 and the light source 103, may be bolted. The mounting plate 107 may be made of wood, a thermosetting mate rial, a polymer, metal or the like. The mounting surface 109 may be shaped complementary to a shape of an inner surface or a portion of an inner surface of the rotor blade. The image acquisition assembly 100 further comprises a control board and/or communication interface 113 which may perform to con trol the camera 101 and/or the light source and which may al so perform some processing of data, such as image data ac quired by the camera 101.

A single image acquisition unit with multiple sensors or cam eras may cover different angles and may ensure that at least or more than 180° will be covered. An illustration of the viewing ranges of three cameras is schematically illustrated in Fig. 2 in a cross-section as viewed along a longitudinal direction 215 of the rotor blade. Therein, (a portion of) the rotor blade wall 217 is schematically illustrated having an inner surface 219 and an outer surface 221 which may be an airfoil of the rotor blade 220. The image acquisition unit 200 is mounted at a portion of the inner surface 219 of the rotor blade and comprises in the illustrated example three cameras having three overlapping viewing ranges 223a, 223b, 223c. The viewing ranges 223a, b,c are in the illuminated ex ample each 36°. As can be taken from Fig. 2, the three camer as are oriented to have viewing directions 225a, 225b, 225c differing by 32°. Since their viewing angle is 36° each, im ages acquired by the three cameras will overlap in an angle range of 4°, wherein the overlap is indicated with reference sign 227. In other embodiments a combined viewing range may cover 180°.

Fig. 3 schematically illustrates in a perspective view a por tion of a rotor blade 320 according to an embodiment of the present invention having installed therein two acquisition units 300a and 300b each comprising three cameras and one or more light sources. The rotor blade is schematically illus trated in a partly broken away form as having a rotor blade wall 317 having an inner surface 319 and having an outer sur- face 321. Each of the two cameras installed in the image ac quisition unit 300a has in the illustrated example a viewing range of 49.2°. The two cameras are oriented such that an overlap of 30° is achieved.

According to an embodiment of the present invention the moni toring system may comprises an image-sensor (e.g. including a lens/obj ective) that covers the 180°. In principle this could be done with a single image sensor (having e.g. a lens) but the quality may be too poor.

When more image sensors (e.g. with lenses) are used to cover the 180° it is important that there exist an overlap (margin) between viewing ranges of the individual image sensors.

The second image acquisition unit 300b has its two or three cameras oriented such that their viewing area 302b (composed of viewing areas 330bl, 330b2 of the two cameras) partly overlaps with the viewing area 302a (composed of viewing are as 330al, 330a2 of the two cameras) of the first image acqui sition unit 300a. According to an embodiment of the present invention, within the viewing areas 302a, 302b, further image acquisition units may be installed which may then monitor the opposite side, thus, the inner surface where the image acqui sition units 300a and 300b are mounted.

Fig. 4 schematically illustrates an elevational view in which the longitudinal direction 415 of the rotor blade is in the horizontal direction. A first image acquisition unit 400a and a second image acquisition unit 400b are installed inside the rotor blade spaced apart by a distance 1 in the longitudinal direction 415. Each of the image acquisition units 400a, 400b comprises three cameras, a first one having the viewing range 231al, another one having the viewing range 231a2 and the third one having the viewing range 231a3. The first camera of the second image acquisition unit 400b has a viewing range 231bl, a second camera has a viewing range 231b2 and a third has a viewing range 231b3. Thereby, the union of all viewing ranges 231al to 231b3 covers substantially entirely the inner surface of one side of the rotor blade.

Fig. 5 schematically illustrates in a perspective view anoth er rotor blade 520 according to an embodiment of the present invention having image acquisition units 500a, 500b arranged inside the rotor blade at different positions spaced apart along the longitudinal direction 515. Thereby, each of the image acquisition units 500a, 500b comprises two cameras hav ing different viewing ranges 530al, 530a2 for the first image acquisition unit 500a. Further, the two cameras of the second image acquisition unit 500b have the viewing ranges 530bl and 530b2 overlapping by several degrees.

Fig. 6 schematically illustrates a rotor blade 620 according to another embodiment of the present invention having several image acquisition units 600a, 600b installed within the rotor blade and having two cameras each monitoring overlapping viewing ranges.

Fig. 7 schematically illustrates a method diagram of a method 740 of monitoring a structural state of a rotor blade of a wind turbine according to an embodiment of the present inven tion. Thereby, the method uses at least one camera mounted inside the rotor blade to acquire at least one image of a portion of an inner surface of the rotor blade. Further, the image is analyzed to determine the structural state of the rotor blade.

According to the embodiment illustrated in Fig. 7 in a method step 741, pictures are captured for example at a daily basis. In a decision block 743 it is checked whether the operation was acceptable and the image quality is sufficient. If the decision block 743 results in "yes" it is proceeded to the method step 745 where feature extraction and/or data pro cessing is performed. In a decision block 747 it is checked, whether the data processing resulted in a value which is smaller or larger than a threshold. If the value is not smaller than the threshold, it is proceeded to method block 749 where a counter is increased which counts the number of warnings. In a decision block 751 it is checked whether the number of warnings is smaller than a threshold. If this is not the case, it is proceeded to method step 753, wherein an alarm is raised.

If the number of warnings is smaller than the threshold, it is recycled back to the first method step 741.

If the decision block 743 found that the operation and quali ty is not acceptable, it is proceeded to method block 755 where no actions are performed and it is cycled back to the first method step 741.

If the decision block 747 found that the value is smaller than the threshold, it is proceeded to the method step 757 where no further actions are taken and it is cycled back to the first method step 741.

As can be taken from Fig. 2, the three cameras cover a range of 180°, i.e. one side of an inner surface of the rotor blade. The remaining 180° may be covered by a similar acqui sition unit sitting on the opposite side of the internal sur face. Together two units sitting opposite to each other may be referred to a set of image acquisition units. For covering the full length of interest of the blade, sets of image ac quisition units may be placed along the blade, such as is il lustrated in Fig. 3.

According to embodiments of the present invention, the images or pictures which have been acquired by the different cameras may be transferred to a diagnostic center or control module or processing module where they may be analyzed in an auto mated manner for damages of the blade. If damages are recog nized, an alarm may be raised, as is indicated in method step 753 in Fig. 7. The analysis may involve feature extraction and may be based on image processing, especially image seg- mentation, for example background subtraction. The images may be compared to known healthy (base line) images or reference images of the internal rotor blades and an alarm may be raised if a threshold is reached, such as the difference of acquired image and reference image shows a pronounced image feature. The diagnostic center could be in-situ at the tur bine level (real-time/online) or on a remote server (of fline) . The method illustrated in Fig. 7 may be applied to all rotor blades of the wind turbine, for example three rotor blades .

Embodiments of the present invention may provide several ad vantages :

- Pictures of the internal surface of the rotor blade may be acquired remotely. This may be an extensive cost re duction as the same operation requires at least two trained maintenance personnel and transportation to sites on a regular basis.

- The option of making an automated analysis of the pic tures and activating alarms when a potential damage is discovered

- Automated procedures using image processing may be ob jective in their detection and such that the detection of the damages does not depend on the specialists knowhow and experience

- Rotor blades according to embodiments of the present in vention may comprise permanently internally mounted units, containing multiple camera units and at least one light source. Identical pictures on a regular basis may be taken, thereby the same viewing angles and light con ditions may be applied. Embodiments of the present in vention may allow a higher likelihood of discovering damages on an early stage, giving lower repair cost and reduction of the risk of a fatal failure. Fig. 8 schematically illustrates a wind turbine 760 according to an embodiment of the present invention. The wind turbine comprises a wind turbine tower 761 at which a nacelle 763 is mounted. The nacelle harbours a generator 765 having a rota tion shaft 767 which is coupled to a hub 769 at which plural rotor blades 720 are mounted, such as rotor blades illustrat ed in one of Figs. 2, 3, 4, 5, 6. An analysis module 771 is arranged within the nacelle 763 and comprises image pro cessing capability to process the image taken by the camera within the rotor blade 720 to recognize features in the image indicating damage of the inner surface of the rotor blade 720.

It should be noted that the term "comprising" does not ex clude other elements or steps and "a" or "an" does not ex clude a plurality. Also elements described in association with different embodiments may be combined. It should also be noted that reference signs in the claims should not be con strued as limiting the scope of the claims.

Claims

1. Rotor blade (220, 320, 420, 520, 620, 720) for a wind tur bine (760), comprising:

at least one camera (101) mounted inside the rotor blade and adapted to acquire an image of a portion of an inner sur face (219) of the rotor blade (220) .

2. Rotor blade according to the preceding claim, further com prising :

at least one light source (103) mounted inside the rotor blade, adapted to generate illumination light and arranged to illuminate the portion of the inner surface (219) .

3. Rotor blade according to any of the preceding claims, wherein the at least one camera (101) and/or the at least one light source (103) is mounted at a mounting portion of the inner surface (219),

wherein the at least one camera and/or the at least one light source is in particular mounted using an adhesive.

4. Rotor blade according to any of the preceding claims, wherein the at least one camera (101) and/or the at least one light source (103) is mounted on at least one frame (105) that is mounted on the inner surface (219) .

5. Rotor blade according to any of the preceding claims, wherein the frame (105) has a mounting surface (109) fit, in particular complementary, to a shape of the mounting portion of the inner surface (219) .

6. Rotor blade according to any of the preceding claims, wherein the at least one camera comprises plural cameras mounted inside the rotor blade and adapted to acquire plural images of plural, in particular partly overlapping, portions (330al, 330a2, 330bl, 330b2) of the inner surface of the ro tor blade, wherein the light source (101) comprises plural light sources mounted inside the rotor blade and arranged to illuminate the plural portions of the inner surface.

7. Rotor blade according to any of the preceding claims, wherein at least one image acquisition unit (100, 200, 300a, 300b, 400a, 400b, 500a, 500b, 600a, 600b) is formed by an as sembly of at least one camera, in particular three cameras, at least one light source all mounted on one frame,

wherein the rotor blade in particular comprises plural image acquisition units, further in particular arranged in sets of image acquisition units mounted to face each other.

8. Rotor blade according to any of the preceding claims, wherein cameras on one image acquisition unit:

are oriented to have viewing directions (225a, 225b,

225c) differing by at least 20°, in particular by between 25° and 70°, further in particular by between 35° and 40°, and/or mounted close to each other.

9. Rotor blade according to any of the preceding claims, wherein the mounting portion of the inner surface (219) is a back surface of an airfoil portion (221) of the rotor blade (220) .

10. Rotor blade according to any of the preceding claims, wherein the plural portions of the inner surface essentially cover an entire longitudinal extent of the rotor blade.

11. Rotor blade according to any of the preceding claims, wherein the at least one camera (101) is sensitive to at least a portion of visual light and/or to at least a portion of infrared light and/or to at least a portion of ultraviolet light .

12. Rotor blade according to any of the preceding claims, further comprising: a wireless or wire based communication interface (113) for communicating control signals and/or image data between the at least one camera and/or the at least one light source and a control module outside the rotor blade.

13. Rotor blade monitoring system, comprising:

a rotor blade (720) according to any of the preceding claims; and

an analysis module (771) comprising image processing ca pability to process the image to recognize features in the image indicating damage of the inner surface.

14. Wind turbine (760) comprising:

a rotation shaft (767); and

a rotor blade (720) according to any of the preceding claims 1 to 12 or a rotor blade monitoring system according to the preceding claim,

wherein the rotor blade (720) is mounted at the rotation shaft (767) .

15. Method of monitoring a structural state of a rotor blade of a wind turbine, the method comprising:

using at least one camera mounted inside the rotor blade to acquire (741) at least one image of a portion of an inner surface (219) of the rotor blade (220); and

analysing (743, 745, 747) the image to determine the structural state of the rotor blade.